Research Catalog

Three dimensional solution of pneumatic active control of forebody vortex asymmetry

Title
Three dimensional solution of pneumatic active control of forebody vortex asymmetry [microform] / Osama A. Kandil and Hazem H. Sharaf El-Din, C.H. Liu.
Author
Kandil, Osama A.
Publication
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Sharaf El-Din, Hazem H.
  • Liu, C. H. (Chen-Huei), 1941-
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-203089
Subject
  • Angle of attack
  • Finite volume method
  • Flux difference splitting
  • Forebodies
  • Navier-stokes equation
  • Pneumatic control
  • Tangential blowing
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 97-0824-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:203089
OCLC
marcive38860601
Author
Kandil, Osama A.
Title
Three dimensional solution of pneumatic active control of forebody vortex asymmetry [microform] / Osama A. Kandil and Hazem H. Sharaf El-Din, C.H. Liu.
Imprint
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA contractor report ; NASA CR-203089
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
Sharaf El-Din, Hazem H.
Liu, C. H. (Chen-Huei), 1941-
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:203089
Research Call Number
READEX Microfiche NAS 1.26:203089
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